Internet Archive Search: creator:"Moore, Royce D"

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	Noise trends of a 0.5 m (20 in.) diameter supersonic throughflow fan as measured in an unmodified compressor aerodynamic test facility - Dittmar, James H. The tone noise levels of a supersonic throughflow fan were measured at subsonic and supersonic axial duct Mach numbers. The noise in the inlet plenum showed no blade passing and harmonic tones at subsonic or supersonic axial flow conditions. At subsonic axial flow conditions, the supersonic throughflow fan showed no inlet plenum tones at fan operating conditions where tone noise had been previously measured for a subsonic fan design... Keywords: AEROSPACE ENGINEERING; DATA BASES; REMOTE SENSING; REMOTE SENSORS; DATA SYSTEMS; EARTH SCIENCES; LABORATORIES; RESEARCH AND DEVELOPMENT; SYSTEMS ENGINEERING; TECHNOLOGY UTILIZATION; AIRBORNE EQUIPMENT; BATHYMETERS Downloads: 42
	Aerodynamic performance of axial-flow fan stage operated at nine inlet guide vane angles - Moore, Royce D "September 1979"--Cover Keywords: Fans (Machinery); Turbomachines Downloads: 14